| Thermal design verification testing of the anchored interplanetary monitoring platform "D" by Jere W. Medlin, United States. National Aeronautics and Space Administration - 1967 - 23 pages |
| Thermal dynamic modeling study by I. U. Ojalvo, Grumman Aerospace Corporation, Langley Research Center - 1972 - 64 pages |
| Thermal energy storage experiments by Lewis Research Center. Space Experiments Division - 1995 - 3 pages |
| Thermal feasibility of using methane or hydrogen fuel for direct cooling of a first-stage turbine stator by Raymond Strong Colladay, United States. National Aeronautics and Space Administration, Lewis Research Center - 1970 - 24 pages |
| Thermal integration of electric power and life support systems for manned space stations by R. W. Woods, E. P. Erlanson - 1966 - 315 pages |
| Thermal pollution analysis - 1975 - 293 pages |
| Thermal response of Space Shuttle wing during reentry heating by L. Gong - 1984 - 18 pages |
| Thermal stratification potential in rocket engine coolant channels by Kenneth J. Kacynski, United States. National Aeronautics and Space Administration. Scientific and Technical Information Program - 1992 - 11 pages |
| Thermal stratification potential in rocket engine coolant channels by Kenneth J. Kacynski - 1992 - 11 pages |
| Thermal stress analysis of ceramic gas-path seal components for aircraft turbines by Francis E. Kennedy, Robert C. Bill, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, Lewis Research Center - 1979 - 19 pages |
| Thermal stress analysis of ceramic gas-path seal components for aircraft turbines by Francis E. Kennedy, Robert C. Bill, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, Lewis Research Center - 1979 - 19 pages |
| Thermal structures and materials for high-speed flight by American Institute of Aeronautics and Astronautics - 1992 - 547 pages |
| Thermal-hydraulics for Space Power, Propulsion, and Thermal Management System Design by William J. Krotiuk - 1990 - 341 pages |
| Thermal-hydraulics for space power, propulsion, and thermal management system design by William J. Krotiuk - 1990 - 341 pages |
| Thermal-structural design study of an airframe-integrated scramjet by O. A. Buchmann, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Langley Research Center - 1979 - 34 pages |
| Thermal-structural design study of an airframe-integrated scramjet by O. A. Buchmann, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Langley Research Center - 1979 - 34 pages |
| Thermal-vacuum testing of high-temperature electrical components by W. L. Grant, P. E. Kueser, Westinghouse Electric Corporation. Aerospace Electrical Division, Lewis Research Center - 1970 - 253 pages |
| Thermionic emission from cesium-coated electrostatic ion-thruster electrodes by Thaine W. Reynolds, Edward A. Richley, United States. National Aeronautics and Space Administration, Lewis Research Center - 1963 - 33 pages |
| Thermodynamic properties of coolant fluids and particle seeds for gaseous nuclear rockets by R. Roback, United States. National Aeronautics and Space Administration, United Aircraft Corporation - 1965 - 22 pages |
| Thermoluminescent spectra of sodium chloride and hydroxide-free sodium chloride irradiated with 40-Mev alpha particles by James A. Partridge, United States. National Aeronautics and Space Administration, Lewis Research Center - 1963 - 15 pages |
| Thermophysical aspects of re-entry flows by James N. Moss, Carl D. Scott, American Institute of Aeronautics and Astronautics - 1986 - 626 pages |
| Thermophysical properties of selected aerospace materials by Purdue University. Thermophysical and Electronic Properties Information Center, Yeram Sarkis Touloukian, Cho Yen Ho - 1976 |
| Thermophysical properties of solid materials by Armour Research Foundation (U.S.), Alexander Goldsmith - 1959 |
| Thermophysics and spacecraft thermal control by Robert G. Hering - 1974 - 551 pages |
| Thermophysics and temperature control of spacecraft and entry vehicles by American Institute of Aeronautics and Astronautics. Thermophysics Committee - 1966 - 867 pages |
| Thermophysics of atmospheric entry by American Institute of Aeronautics and Astronautics - 1982 - 521 pages |
| Thermophysics of spacecraft and planetary bodies by American Institute of Aeronautics and Astronautics - 1967 - 975 pages |
| Thermophysics of spacecraft and planetary bodies by American Institute of Aeronautics and Astronautics - 1967 - 975 pages |
| Thin sheet impact by C. J. Maiden, A. R. McMillan, R. E. Sennett - 1965 - 57 pages |
| Things that fly by Huck Scarry - 1986 - 42 pages |
| Thinks-I-to-myself by Edward Nares - 1812 - 215 pages |
| Third Annual Workshop on Space Operations Automation and Robotics ((SOAR '89) by Sandy Griffin, United States. National Aeronautics and Space Administration, United States. Air Force, University of Houston--Clear Lake - 1990 - 701 pages |
| Third International Conference on Spacecraft Propulsion by European Space Agency - 2000 - 936 pages |
| Third party damage by aircraft by James Molony Spaight - 1939 - 26 pages |
| Thirteen: the flight that failed by Henry S. F. Cooper - 1972 - 199 pages |
| Thirty-sixth Annual General Meeting Canadian Aeronautics and Space Institute by Canadian Aeronautics and Space Institute. General Meeting, Canadian Aeronautics and Space Institute - 1990 |
| This flying game by Henry Harley Arnold, Ira Eaker - 1943 - 327 pages |
| This flying game by Henry Harley Arnold, Ira Eaker - 1943 - 327 pages |
| This flying game by Henry Harley Arnold, Ira Eaker - 1938 - 307 pages |
| This flying game by Henry Harley Arnold, Ira Eaker - 1936 - 275 pages |
| Thornycroft road transport golden jubilee by Richard Twelvetrees - 1946 - 95 pages |
| Those wonderful women in their flying machines by Sally Van Wagenen Keil - 1979 - 334 pages |
| Thoughts on the history of U. S. transport airplanes by William Littlewood - 1964 - 64 pages |
| Threats, Risks and Sustainability - Answers by Space - 2009 - 321 pages |
| Three and four coil systems for homogeneous magnetic fields by M. E. Pittman, Donald Long Waidelich, Goddard Space Flight Center - 1964 - 16 pages |
| Three ballistic camera data reduction methods applicable to reentry experiments by John E. Hogge, United States. National Aeronautics and Space Administration, Langley Research Center - 1967 - 40 pages |
| Three Decades to a Space Shuttle by D. M. Wylie - 2004 - 201 pages |
| Three input concepts for flight crew interaction with information presented on a large-screen electronic cockpit display by Denise R. Jones, Langley Research Center - 1990 - 24 pages |
| Three input concepts for flight crew interaction with information presented on a large-screen electronic cockpit display by Denise R. Jones, Langley Research Center - 1990 - 24 pages |
| Three methods of presenting flight vector information in a head-up display during simulated STOL approaches by James H. Dwyer, Everett A. Palmer, Ames Research Center - 1975 - 15 pages |
| Three methods of presenting flight vector information in a head-up display during simulated STOL approaches by James H. Dwyer, Everett A. Palmer, Ames Research Center - 1975 - 15 pages |
| Three-dimensional trajectory analyses of two drop sizing instruments by Hillyer G. Norment, Lewis Research Center, United States. Dept. of Transportation - 1988 - 60 pages |
| Three-step labyrinth seal for high-performance turbomachines by Robert C. Hendricks - 1987 - 74 pages |
| Throat stability-bypass systems to increase the stable airflow range of a Mach 2.5 inlet with 60-percent internal contraction by Glenn A. Mitchell, Bobby W. Sanders, Robert Joseph Shaw, Lewis Research Center - 1974 - 41 pages |
| Throttle Full Open by Jane Falloon - 1999 - 215 pages |
| Thrust and wing loading requirements for short haul aircraft constrained by engine noise and field length by Jeffrey V. Bowles, Mark H. Waters, Thomas L. Galloway, Ames Research Center - 1976 - 36 pages |
| Thrust measurement of Space Electric Rocket Test I ion thrustors by William C. Nieberding, Robert R. Lovell, United States. National Aeronautics and Space Administration, Lewis Research Center - 1966 - 41 pages |
| Thrust measurements of a hollow-cathode discharge by Aaron Snyder, Bruce A. Banks, United States. National Aeronautics and Space Administration, Lewis Research Center - 1972 - 18 pages |
| Thrust performance of a variable-geometry, nonaxisymmetric, two-dimensional, convergent-divergent exhaust nozzle on a turbojet engine at altitude by David M. Straight, Richard R. Cullom, Lewis Research Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch - 1983 - 36 pages |
| Thrust performance of isolated 36-chute suppressor plug nozzles with and without ejectors at Mach numbers from 0 to 0.45 by Douglas E. Harrington, James J. Schloemer, Stanley Andrew Skebe, Lewis Research Center - 1975 - 44 pages |
| Thrust performance of isolated 36-chute suppressor plug nozzles with and without ejectors at Mach numbers from 0 to 0.45 by Douglas E. Harrington, James J. Schloemer, Stanley Andrew Skebe, Lewis Research Center - 1975 - 44 pages |
| Thrust performance of isolated plug nozzles with two types of 40-spoke noise suppressor at Mach numbers from 0 to 0.45 by Douglas E. Harrington, James J. Schloemar, Lewis Research Center - 1974 - 35 pages |
| Thrust performance of isolated two dimension suppressed plug nozzles with and without ejectors at mach numbers from 0 to 0.45 by Douglas E. Harrington, James J. Schloemer, Stanley A. Skebe, Lewis Research Center, United States. National Aeronautics and Space Administration - 1976 - 35 pages |
| Thrust vectoring on the NASA F-18 high alpha research vehicle by Albion H. Bowers, Joseph W. Pahle, United States. National Aeronautics and Space Administration. Scientific and Technical Information Division - 1996 - 34 pages |
| Tie-down sense by United States. Federal Aviation Administration - 1968 |
| Time required for an adequate thermal-vacuum test of flight model spacecraft by A. R. Timmins, United States. National Aeronautics and Space Administration, Goddard Space Flight Center - 1968 - 19 pages |
| Time-dependent polar distribution of outgassing from a spacecraft by John J. Scialdone, Goddard Space Flight Center - 1974 - 20 pages |
| Tire tread temperatures during antiskid braking and cornering on a dry runway by John A. Tanner, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, Langley Research Center - 1982 - 54 pages |
| Tire-to-surface friction-coefficient measurements with a C-123B airplane on various runway surfaces by Richard H. Sawyer, Joseph J. Kolnick - 1959 - 32 pages |
| Titanium alloys by Vydehi Arun Joshi - 2006 - 227 pages |
| Titanium and titanium alloy fasteners by Northrop Corporation, J. L. Chinn, United States. Air Force. Air Matériel Command - 1958 |
| Titanium and titanium alloy fasteners by J. L. Chinn - 1958 |
| Titanium and titanium alloy fasteners by Northrop Corporation, J. L. Chinn, United States. Air Force. Air Matériel Command - 1958 |
| To amend the Federal aviation act of 1958 relating to emergency locator transmitters by United States. Congress. House. Committee on Public Works and Transportation. Subcommittee on Aviation - 1976 - 38 pages |
| To amend the Federal aviation act of 1958 relating to emergency locator transmitters by United States. Congress. House. Committee on Public Works and Transportation. Subcommittee on Aviation - 1976 - 38 pages |
| To authorize the Coast Guard to operate and maintain ocean stations by United States. Congress. House. Committee on Merchant Marine and Fisheries. Subcommittee on Coast Guard, Coast and Geodetic Survey, and Public Health Service - 1947 - 82 pages |
| To review the status of the airborne traffic alert and collision avoidance system (TCAS) by United States. Congress. House. Committee on Public Works and Transportation. Subcommittee on Investigations and Oversight - 1992 - 101 pages |
| To review the status of the airborne traffic alert and collision avoidance system (TCAS) by United States. Congress. House. Committee on Public Works and Transportation. Subcommittee on Investigations and Oversight - 1992 - 101 pages |
| To the end of the solar system by James A. Dewar - 2004 - 438 pages |
| Together in orbit by John M. Logsdon, United States. National Aeronautics and Space Administration. History Office - 1998 - 52 pages |
| Together in orbit by John M. Logsdon, United States. National Aeronautics and Space Administration. History Office - 1998 - 52 pages |
| Torque and leakage rates of various lubricated lip seal designs at a peripheral velocity of 120 feet per second by Lawrence P. Ludwig, Thomas N. Strom, Robert L. Johnson, Lewis Research Center, United States. National Aeronautics and Space Administration - 1969 - 14 pages |
| Torquing of nuts in aircraft engines by Society of Automotive Engineers. War Engineering Board - 1943 |
| Torquing of nuts in aircraft engines by Society of Automotive Engineers. War Engineering Board - 1943 - 109 pages |
| Torsional instabilities in composite and composite-reinforced aluminum-alloy thin-walled cylinders by Donald E. Marlowe - 1972 - 72 pages |
| Torsional instabilities in composite and composite-reinforced aluminum-alloy thin-walled cylinders by Donald E. Marlowe - 1972 - 72 pages |
| Torsional shear strength of filament-wound glass-epoxy tubes by L. David Wall (Jr.), Michael F. Card, United States. National Aeronautics and Space Administration, Langley Research Center - 1971 - 46 pages |
| Torsional vibration characteristics of a 1/5-scale model of Saturn SA-1 by John J. Catherine, United States. National Aeronautics and Space Administration - 1965 - 53 pages |
| Tory II-A mechanical and aero-thermodynamic design by J. W. Cox, University of California, Livermore. Lawrence Radiation Laboratory, U.S. Atomic Energy Commision, United States. Energy Research and Development Administration - 1962 - 47 pages |
| Total energy-rate feedback for automatic glide-slope tracking during wind-shear penetration by Christine M. Belcastro, Aaron J. Ostroff, Langley Research Center - 1985 - 69 pages |
| Tough composite materials by Louis F. Vosteen, Norman Joseph Johnston, Louis A. Teichman - 1984 - 391 pages |
| Toward a science of command, control, and communications by Carl R. Jones - 1993 - 284 pages |
| Toward Mach 2 by J. D. Hunley - 1999 - 161 pages |
| Toys in space by Carolyn Sumners - 1994 - 141 pages |
| Tracking systems, their mathematical models and their errors by F. O. Vonbun, Werner D. Kahn, Goddard Space Flight Center, United States. National Aeronautics and Space Administration - 1962 - 46 pages |
| Tracking systems: their mathematical models and their errors by Werner D. Kahn, F. O. Vonbun - 1966 |
| Trade-off study and conceptual designs of regenerative advanced integrated life support systems (AILSS) by United Aircraft Corporation. Hamilton Standard Division, Langley Research Center - 1970 - 755 pages |
| Trade-off study and conceptual designs of regenerative advanced integrated life support systems (AILSS) by United Aircraft Corporation. Hamilton Standard Division, Langley Research Center - 1970 - 755 pages |
| Trade-offs arising from mixture of color cueing and monocular, binoptic, and stereoscopic cueing information for simulated rotorcraft flight by Russell V. Parrish, Steven P. Williams, United States. National Aeronautics and Space Administration. Scientific and Technical Information Program - 1993 - 81 pages |
| Traffic by Commission of the European Communities. Directorate-General for Transport - 1999 - 52 pages |
| Tragedy at Tuskar Rock by Mike Reynolds - 2003 - 238 pages |
| Tragflügeltheorie by Élie Carafoli - 1954 - 562 pages |
| Training of civil aircraft pilots by United States. Congress. House. Committee on Interstate and Foreign Commerce - 1939 - 66 pages |
| Traitement en Hongrie d'un avion des Etats-Unis d'Amérique (Etats-Unis d'Amérique c. République Populaire de Hongrie; Etats-Unis Soviétiques) by United States, International Court of Justice - 1954 - 107 pages |
| Traité d'aérostation by Raoul Marquis - 1891 - 267 pages |
| Traité d'aérostation by Raoul Marquis - 1891 - 267 pages |
| Traité d'aérostation by Raoul Marquis - 1891 - 267 pages |
| Trajectory control for vehicles entering the earth's atmosphere at small flight-path angles by John M. Eggleston, John W. Young - 1961 - 29 pages |
| Trajectory optimization for an Apollo-type vehicle under entry conditions encountered during lunar return by John W. Young, Robert Lee Smith - 1967 - 39 pages |
| Trajectory simulation applicable to stability and control studies of large multi-engine vehicles by Ronald J. Harris, George C. Marshall Space Flight Center. Advanced Flight Systems Branch - 1963 - 84 pages |
| Trandes by Leland A. Carlson, United States. National Aeronautics and Space Administration, Texas A & M University - 1977 - 109 pages |
| Trandes by Leland A. Carlson, United States. National Aeronautics and Space Administration, Texas A & M University - 1977 - 109 pages |
| Trandes by Leland A. Carlson, United States. National Aeronautics and Space Administration, Texas A & M University - 1977 - 111 pages |
| Transactions by Society of Automotive Engineers - 1923 |
| Transactions by Society of Automotive Engineers - 1916 |
| Transactions by Society of Automotive Engineers - 1915 |
| Transactions by Society of Automotive Engineers - 1914 |
| Transactions by Society of Automotive Engineers - 1914 |
| Transactions by Society of Automotive Engineers - 1913 |
| Transactions by Society of Automotive Engineers - 1913 |
| Transactions by Society of Automotive Engineers - 1912 |
| Transactions by Society of Automotive Engineers - 1912 |
| Transactions by Society of Automotive Engineers - 1910 |
| Transactions of the ninth Scientific conference of graduate students and junior scientific associates of the Institute for the History of Natural Science and Technology by Institut istorii estestvoznanii︠a︡ i tekhniki (Akademii︠a︡ nauk SSSR), I︠U︡. V. Biri︠u︡kov - 1969 - 55 pages |
| Transactions of the tenth Scientific conference of the Institute of History of Natural Science and Technology by Institut istorii estestvoznanii︠a︡ i tekhniki (Akademii︠a︡ nauk SSSR), Yu. V. Biryukov - 1969 - 62 pages |
| TRANSEP: A program for high lift separated flow about airfoils by L. A. Carlson - 1980 - 56 pages |
| Transfer function approximations for large highly coupled elastic boosters with fuel slosh by R. L. Stapleford - 1966 - 162 pages |
| Transforming and using space-research knowledge, ten diversified views by United States. National Aeronautics and Space Administration, University of California, Los Angeles - 1964 - 110 pages |
| Transient characteristics of a voltage regulator and a parasitic speed controller on a 14.3-kilovolt-ampere, 1200-hertz modified lundell alternator by Heinz L. Wimmer, Bill D. Ingle, United States. National Aeronautics and Space Administration, Lewis Research Center - 1970 - 25 pages |
| Transient shutdown analysis of low-temperature thermal diodes by Richard John Williams, Ames Research Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office - 1979 - 18 pages |
| Transient shutdown analysis of low-temperature thermal diodes by Richard John Williams, Ames Research Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office - 1979 - 18 pages |
| Transient stability analysis of synchronous motors by Jir̆í C̆emus, Václáv Hamata - 1990 - 266 pages |
| Transient stability analysis of synchronous motors by Jir̆í C̆emus, Václáv Hamata - 1990 - 266 pages |
| Transient thermodynamic analysis of a fuel-cell system by William Emile Simon - 1968 - 81 pages |
| Transition fixing for hypersonic flow by James R. Sterrett, Langley Research Center - 1967 - 20 pages |
| Transmission line design for a power distribution system at 20 kHz for aircraft by L. W. Zelby - 1986 - 38 pages |
| Transonic aerodynamic and aeroelastic characteristics of a variable sweep wing by P. M. Goorjian - 1985 - 18 pages |
| Transonic aerodynamic characteristics of a proposed assured crew return capability (ACRC) lifting-body configuration by George M. Ware, Langley Research Center - 1989 - 72 pages |
| Transonic aerodynamic characteristics of a proposed assured crew return capability (ACRC) lifting-body configuration by George M. Ware, Langley Research Center - 1989 - 72 pages |
| Transonic aerodynamic characteristics of a tailless fixed-wing supersonic transport model by Edward J. Ray, Robert T. Taylor, Langley Research Center - 1966 - 75 pages |
| Transonic aerodynamic damping and oscillatory stability in yaw and pitch for a model of a variable-sweep supersonic transport airplane by Bruce R. Wright, Benjamin T. Averett, United States. National Aeronautics and Space Administration - 1966 - 20 pages |
| Transonic aeroelastic analysis of launch vehicle configurations by João Luiz Filgueiras de Azevedo, Langley Research Center - 1988 - 310 pages |
| Transonic aeroelastic analysis of launch vehicle configurations by João Luiz Filgueiras de Azevedo, Langley Research Center - 1988 - 154 pages |
| Transonic airfoil analysis and design in nonuniform flow by J. F. Chang - 1986 - 84 pages |
| Transonic airfoil design using cartesian coordinates by Leland A. Carlson, United States. National Aeronautics and Space Administration, Texas A. and M. Research Foundation - 1976 - 33 pages |
| Transonic airfoil flowfield analysis using Cartesian coordinates by Leland A. Carlson, Texas A and M Research Foundation, Langley Research Center - 1975 - 33 pages |
| Transonic and supersonic flutter trend investigation of a variable-sweep wing by R. C. Goetz - 1961 - 29 pages |
| Transonic and supersonic test of a Mach 2.65 mixed-compression axisymmetric intake by J. L. Koncsek - 1972 - 89 pages |
| Transonic flutter characteristics of a 45° sweptback wing with various distributions of ballast along the leading edge by John R. Unangst, United States. National Aeronautics and Space Administration - 1959 - 32 pages |
| Transonic flutter characteristics of an aspect-ratio-4, 45° sweptback, taper-ratio-0.2 plan form by John R. Unangst, United States. National Aeronautics and Space Administration - 1959 - 29 pages |
| Transonic flutter study of a 50.5 ̊cropped-delta wing with two rearward-mounted nacelles by Maynard C. Sandford, Charles L. Ruhlin, Irving Abel, Langley Research Center - 1974 - 29 pages |
| Transonic off-design drag and performance of three mixed-compression axisymmetric inlets by Richard R. Woollett, Edward T. Meleason, David A. Choby, Lewis Research Center - 1975 - 48 pages |
| Transonic off-design drag and performance of three mixed-compression axisymmetric inlets by Richard R. Woollett, Edward T. Meleason, David A. Choby, Lewis Research Center - 1975 - 48 pages |
| Transonic off-design performance of a fixed divergent ejector designed for a mach number of 2.0 by M. D. Cassetti - 1959 - 62 pages |
| Transonic performance of a Mach 2.65 auxiliary flow axisymmetric inlet by Don M. Santman, Ellco Engineering, Inc, Ames Research Center, United States. National Aeronautics and Space Administration - 1976 - 61 pages |
| Transonic performance of a Mach 2.65 auxiliary flow axisymmetric inlet by Don M. Santman, Ellco Engineering, Inc, Ames Research Center, United States. National Aeronautics and Space Administration - 1976 - 61 pages |
| Transonic pressure distributions over protuberances and adjacent areas in proximity to the nose of a launch vehicle by James A. Blackwell, United States. National Aeronautics and Space Administration, Langley Research Center - 1966 - 32 pages |
| Transonic single-mode flutter and buffet of a low aspect ratio wing having a subsonic airfoil shape by Larry L. Erickson, Ames Research Center - 1974 - 19 pages |
| Transonic wind-tunnel investigation of the fin loads of a 1/8-scale model simulating the first stage of the Scout research vehicle by Thomas C. Kelly, Langley Research Center - 1961 - 28 pages |
| Transonic wind-tunnel investigation of the maneuver potential of the NASA supercritical wing concept by James B. Hallissy, Theodore G. Ayers, United States. National Aeronautics and Space Administration - 1977 - 293 pages |
| Transonic wind-tunnel investigation of the maneuver potential of the NASA supercritical wing concept by James B. Hallissy, Theodore G. Ayers, United States. National Aeronautics and Space Administration - 1977 - 293 pages |
| Transonic wind-tunnel investigation of the static aerodynamic characteristics of several configurations of the Blue Scout launch vehicle by Thomas C. Kelly, Robert J. Keynton, Langley Research Center - 1963 - 41 pages |
| Transport airplane accidents, hazards and malfunctions, scheduled domestic and foreign/overseas passenger operations, July 1, 1947 through December 31, 1954 by United States. Civil Aeronautics Board, Hugh B. Freeman - 1956 - 14 pages |
| Transport composite fuselage technology: Impact dynamics and acoustic transmission by A. C. Jackson - 1986 - 163 pages |
| Transport dynamics of a high-power-density matrix-type hydrogen-oxygen fuel cell by Paul R. Prokopius, Norman H. Hagedorn, Lewis Research Center - 1974 - 18 pages |
| Transport research by European Commission - 1998 |
| Treatment in Hungary of aircraft and crew of United States of America by International Court of Justice - 1958 - 87 pages |
| Trends in the development of automatic test equipment by Jack Lustig, David Marshall Goodman - 1973 - 344 pages |
| Tripwired? Document Trail of Faulty Airplane Wiring Demonstrates Need for Comprehensive Review - 1998 - 94 pages |
| Turbine aerodynamic and cooling requirements for a turbojet powered Mach 3 transport using methane fuel by David G. Evans, Keith A. Furgalus, Francis S. Stepka, United States. National Aeronautics and Space Administration, Lewis Research Center - 1970 - 78 pages |
| Turbine design and application - 1972 |
| Turbine design and application - 1972 |
| Turbine for a low-cost turbojet engine by Milton G. Kofskey, Lewis Research Center, U.S. Army Air Mobility Research and Development Laboratory - 1974 |
| Turbine- and jet-propelled aircraft powerplants by James P. Eames - 1954 - 237 pages |
| Turbine- and jet-propelled aircraft powerplants by James P. Eames - 1954 - 237 pages |
| Turbofan forced mixer lobe flow modeling by T. Barber, Lewis Research Center - 1988 |
| Turbofan forced mixer lobe flow modeling by T. Barber, Lewis Research Center - 1988 |
| Turbojet combustor performance with natural gas fuel by Nicholas R. Marchionna, Arthur M. Trout, Lewis Research Center - 1970 - 33 pages |
| Turbojet fundamentals by Howard E. Morgan - 1956 - 87 pages |
| Turbojet-exhaust-nozzle secondary-airflow pumping as an exit control of an inlet-stability bypass system for a Mach 2.5 axisymmetric mixed-compression inlet by Bobby W. Sanders, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, Lewis Research Center - 1980 - 78 pages |
| Turbojet-exhaust-nozzle secondary-airflow pumping as an exit control of an inlet-stability bypass system for a Mach 2.5 axisymmetric mixed-compression inlet by Bobby W. Sanders, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, Lewis Research Center - 1980 - 78 pages |
| Turbojet-ramjet propulsion system for all-body hypersonic aircraft by Mark H. Waters, United States. National Aeronautics and Space Administration - 1971 - 49 pages |
| Turboprop engines by P. K. Kazandzhan, Andreĭ Vasilʹevich Kuznet︠s︡ov - 1963 - 341 pages |
| Turbulence and longitudinal flying qualities by James A. Franklin, Princeton University, United States. National Aeronautics and Space Administration - 1971 - 147 pages |
| Twelve walked away by Marguerite Gaylord Tate - 1948 - 150 pages |
| Twenty year cumulative index, 1951-1971 - 1972 - 121 pages |
| Twenty-five years of the American Astronautical Society by Eugene Morlock Emme - 1980 - 236 pages |
| Twenty-five years of the American Astronautical Society - 1980 - 236 pages |
| Twenty-five years of the American Astronautical Society by Eugene Morlock Emme - 1980 - 236 pages |
| Two degree-of-freedom flutter solution for a personal computer by D. L. Turnock - 1985 - 43 pages |
| Two dimensional inviscid jet flow from two nozzles at an angle to a plane surface by Marvin E. Goldstein, Robert Siegel, United States. National Aeronautics and Space Administration, Lewis Research Center - 1969 - 42 pages |
| Two experimental supercritical laminar-flow-control swept-wing airfoils by Dennis O. Allison - 1987 - 24 pages |
| Two for survival by Arthur J. Roth - 1976 - 169 pages |
| Two sides of the moon by David Scott, Alexei Leonov - 2004 - 415 pages |
| Two sighting problems associated with sextant type measurements for space navigation by Daniel M. Hegarty, Marvin H. Thigpen, United States. National Aeronautics and Space Administration, Ames Research Center - 1963 - 8 pages |
| Two-dimensional wind tunnel test of an oscillating rotor airfoil by Leo U. Dadone, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, Langley Research Center, Boeing Vertol Company - 1977 - 307 pages |
| Two-dimensional wind tunnel test of an oscillating rotor airfoil by Leo U. Dadone, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office - 1977 - 160 pages |
| Two-dimensional wind tunnel test of an oscillating rotor airfoil by Leo U. Dadone, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office - 1977 - 160 pages |
| Two-dimensional wind tunnel test of an oscillating rotor airfoil by Leo U. Dadone, Boeing Vertol Company, Langley Research Center - 1977 |
| Two-layer thermal barrier coating for turbane airfoils - furnace and burner rig test results by Stephan Stecura, Lewis Research Center, United States. National Aeronautics and Space Administration - 1976 - 18 pages |